[0001] The invention relates to a rotary compressor such as a screw-type or a spiral compressor,
comprising a compressor stator and one or more rotary compression elements, which
compressor stator is provided with a suction port, a delivery port and a lubricant
inlet, the lubricant being intended for lubricating each compression element, for
sealing the gaps between the individual compression elements and between the compression
elements and the compressor stator, and for cooling the medium to be compressed during
the compression process, and also comprising a device for cooling the lubricant by
injecting a cooling medium.
[0002] Such a rotary compressor is known from German Patent 2,261,336. In this case the
lubricant, which is discharged from the compressor together with the compressed medium,
is cooled by injecting a cooling medium. Due to the fact that this cooling medium
evaporates in the space in which the mixture is compressed, the temperature of said
mixture falls, which means that the oil temperature also falls.
[0003] This known method of cooling has the disadvantage that cooling medium in liquid form
leaks through the gaps to be sealed with lubricant, as a result of which loss of output
occurs. A second disadvantage is that the cooling medium disrupts the lubrication
of the compression elements during the compression process, which reduces the operating
reliability of the compressor.
[0004] In the absence of a device for cooling the lubricant in the compressor a heat exchanger
is built into the system, taking up quite a large amount of space. This heat exchanger
is then situated between the oil separating device and the lubricant injection point
on the compressor.
[0005] The object of the invention is therefore to provide a compressor of the type mentioned
above, in which optimum cooling of the lubricant is ensured, without the output and
the operating reliability being adversely affected, while the size of the device required
for the purpose can still remain limited. This is achieved through the fact that the
device for cooling the lubricant comprises a cooling medium inlet opening out near
or in the delivery port.
[0006] The compressed mixture leaving the compressor via the delivery port has a high degree
of turbulence. Since the cooling medium is injected precisely at this point, a thorough
mixing of the mixture and the cooling medium is obtained in a short time and over
a short distance. This ensures a rapid and reliable cooling of the mixture through
the evaporating cooling medium. This is necessary to prevent cooling medium from being
discharged in the liquid state into the oil separating device, with the risk of liquid
cooling medium being fed to the compressor instead of lubricant, for example at the
position of the bearings.
[0007] The cooling of the compressed mixture could also take place through injection of
cooling medium liquid at a point downstream of the delivery port. The turbulence will,
however, in that case be much less strong, which is less advantageous for rapid cooling.
[0008] In the known device for cooling the compressed mixture the cooling action can be
improved by generating turbulence in, for example, the delivery pipe between compressor
and oil separator. This is, however, accompanied in most cases by a fall in pressure,
which adversely affects output.
[0009] The invention can be used for any type of rotary compressor. Beneficial results can
be obtained in particular in this respect in the case of a twin-screw compressor which
is provided with a compressor stator with a gastight outer shell and an inner double
cylindrical housing, in which the housing has at least one bore opening out in or
near the delivery port.
[0010] The cooling medium can be fed to the bore by means of a pipe which opens out with
one end on the outside of the shell, and is connected at the other end to the bore.
[0011] Since the shell and the housing of the compressor reach a different temperature during
operation, expansion differences will occur between them. The cooling medium inlet
therefore preferably has a flexible part between shell and housing for absorbing said
expansion differences.
[0012] Particularly good results are obtained if the housing has three bores which are distributed
regularly at an angle of essentially 90° over the half of the housing facing away
from the delivery aperture opening out laterally on the housing. These three bores
mean, on the one hand, that sufficient cooling medium can be fed in while, on the
other, the diameter of the bores can remain limited. This is important for maintaining
the mechanical strength of the housing at a sufficiently high level.
[0013] Each bore preferably runs in a plane at right angles to the axis of rotation of the
compressor elements. This ensures that the injected cooling medium does not go between
said compressor elements, which would adversely affect their operation.
[0014] The invention will be explained in greater detail below with reference to an example
of an embodiment shown in the figures.
[0015] Figure 1 shows a circuit diagram of a cooling plant containing a screw compressor
according to the invention.
[0016] Figure 2 shows a top view, partially in section, of the housing of a twin-screw compressor.
[0017] Figure 3 shows a cross-section III-III according to Figure 2.
[0018] In the diagram shown in Figure 1 the screw compressor according to the invention
is indicated by 1. The cooling medium is compressed by means of this screw compressor
1. The cooling liquid mixed with lubricant passes through the delivery pipe 2 into
the oil separating device 3, in which the lubricant is separated from the gaseous,
compressed cooling medium. The cooling medium then flows through the condenser 4,
in which condensation occurs, following which expansion takes place at 5. Finally,
vaporisation occurs in the cooling element 6, with the result that the desired cooling
effect is obtained. The vaporised, gaseous cooling medium then flows back to the screw
compressor 1, following which the cycle described above is repeated.
[0019] According to the invention, the liquefied cooling medium is now injected through
pipe 7 and pump 8 in or near the delivery port 9 of the screw compressor 1. A very
good mixing of the cooling medium with the mixture supplied through the screw compressor
1, composed of compressed cooling medium and oil, is obtained as a result. The cooling
medium vaporising in the delivery port 9 and fed in through pipe 7 can consequently
exert an excellent cooling influence on the mixture compressed by the screw compressor
1, with the result that already after a length of pipe 2 of one meter the oil has
reached the desired temperature. Oil can be fed to the oil injection points and the
bearings of the compressor by means of oil pump 22.
[0020] Figure 2 shows a cross-section through a twin-screw compressor, at the level of the
compression elements 10, 11 in the form of screws. The screw compressor has an outer
shell 12 and an inner double cylindrical housing 13, which are rigidly connected to
each other. The screws 10 and 11 are supported in the known manner and are also driven
in the known manner by shaft 14. The arrows 15 indicate the infeed of the medium to
be compressed, and the arrow 16 indicates the discharge. Of course, the medium to
be compressed is sucked in through the suction port and is discharged from the screw
compressor through the delivery port, which is shown schematically at 17. As further
shown in Figure 2, feed elements 18 open out in this delivery port 17, through which
elements a cooling medium for cooling the compressed mixture coming out of the screw
compressor and also containing oil is fed in.
[0021] Figure 3 shows more clearly how these elements 18 are fitted. Bores 19 are first
provided for the purpose in the double cylindrical housing 13, which bores open out
into the delivery port 17 at one side and onto the outside of said double cylindrical
housing at the other side. A pipe 20 is connected there to each bore, said pipe opening
out via a screw coupling 21 onto the outside of the outer shell 12 of the screw compressor.
[0022] The cooling medium can be injected by means of the feed elements 18 into the delivery
port, where the compressed mixture, which also contains oil, is in a very turbulent
state. This means that the cooling medium is directly mixed with that mixture, with
the result that a good heat exchange is obtained.
[0023] The pipes 20 can be flexible, in order to ensure that expansion differences between
the outer shell 12 and the double cylindrical housing 13 cannot lead to breakage.
1. Rotary compressor such as a screw-type or a spiral compressor, comprising a compressor
stator and one or more rotary compression elements, which compressor stator is provided
with a suction port, a delivery port and a lubricant inlet, the lubricant being intended
for lubricating each compression element, for sealing the gaps between the individual
compression elements and between the compression elements and the compressor stator,
and for cooling the medium to be compressed during the compression process, and also
comprising a device for cooling the lubricant by injecting a cooling medium, characterised in that the device for cooling the lubricant comprises a cooling medium inlet opening out
near or in the delivery port.
2. Twin-screw compressor according to Claim 1, provided with a compressor stator with
a gastight outer shell and an inner double cylindrical housing, in which the housing
has at least one bore opening out in or near the delivery port.
3. Twin-screw compressor according to Claim 2, in which the shell has at least one pipe
opening out on its outside and connected to the bore.
4. Twin-screw compressor according to Claim 3, in which the cooling medium inlet has
a flexible part between shell and housing for absorbing expansion differences.
5. Twin-screw compressor according to any of Claims 2 - 4, in which the housing has three
bores which are distributed regularly at an angle of essentially 90° over the half
of the housing facing away from the delivery aperture opening out laterally on the
housing.
6. Twin-screw compressor according to any of Claims 2 - 5, in which each bore runs in
a plane at right angles to the axis of rotation of the compressor elements.